High-strength hot-rolled steel sheet excelling in bore expandability and ductility and process for producing the same

ABSTRACT

This invention provides a high-strength hot-rolled steel sheet having strength of at least  980  N/mm 2  at a sheet thickness of from about 1.0 to about 6.0 mm and excellent in hole expandability, ductility and ability of phosphate coating, which steel sheet is directed to automotive suspension components that are subjected to pressing. The high-strength hot-rolled steel sheet contains, in terms of a mass %, C: 0.01 to 0.09%, Si: 0.05 to 1.5%, Mn: 0.5 to 3.2%, Al: 0.003 to 1.5%, P: 0.03% or below, S: 0.005% or below, Ti: 0.10 to 0.25%, Nb: 0.01 to 0.05% and the balance consisting of iron and unavoidable impurities; satisfies all of the following formulas &lt;1&gt;to &lt;3&gt;: 
 
0.9≦48/12×C/Ti&lt;1.7  &lt;1&gt;
 
50,227×C−4,479×Mn&gt;−9,860  &lt;2&gt;
 
811×C+135×Mn+602×Ti+794×Nb&gt;465  &lt;3&gt;, 
 
and has strength of at least  980  N/mm 2 .

TECHNICAL FIELD

This invention relates to a high-strength hot-rolled steel sheet, directed to automotive suspension components mainly formed by press working, having a strength of at least 980 N/mm² at a sheet thickness of about 1.0 to about 6.0 mm and excellent in hole expandability and ductility, and a production method of the steel sheet.

BACKGROUND ART

The needs for the reduction of the weight of a car body, the integral molding of components and a reduction in the production cost, through rationalization of a production process, have been increased in recent years as means for improving fuel efficiency to cope with the environmental problems caused by automobiles, and the development of high-strength hot-rolled steel sheets having excellent press workability has been carried out. Elongation and hole expandability are particularly important in molding a hot-rolled steel sheet, and Japanese Unexamined Patent Publication (Kokai) Nos. 6-287685, 7-11382 and 6-200351 propose technologies that improve the hole expandability by adjusting the addition amounts of Ti, Nb and C and S to steel sheets having a strength level of 590 to 780 N/mm². However the development of high-strength steel sheets exceeding 980 N/mm² is necessary to satisfy further needs for a reduction in weight. Elongation and hole expandability are deteriorated with an increase in the strength and the hole expandability and ductility are contradictory, as is well known in the art. It has therefore been difficult, using the prior art technologies, to produce steel sheets of the 980 N/mm² level that are excellent in both elongation and hole expandability.

DISCLOSURE OF THE INVENTION

To solve the problems of the prior art described above, the invention contemplates to provide a high-strength hot-rolled steel sheet that can prevent deterioration of hole expandability and ductility with the increase of strength above 980 N/mm² and has high hole expandability and high ductility even when its strength is high, and a production method of such a steel sheet.

The high-strength steel sheet excellent in hole expandability, ductility and ability of phosphate coating, that is intended to solve the problems described above, and its production method, are as follows.

(1) A high-strength hot-rolled steel sheet excellent in hole expandability and ductility, containing in terms of a mass %:

C, 0.01 to 0.09%,

Si: 0.05 to 1.5%,

Mn: 0.5 to 3.2%,

Al: 0.003 to 1.5%,

P: 0.03% or below,

S: 0.005% or below,

Ti: 0.10 to 0.25%,

Nb: 0.01 to 0.05%, and

the balance consisting of iron and unavoidable impurities;

satisfying all of the following formulas <1>to <3>: 0.9≦48/12×C/Ti <1.7  <1> 50,227×C−4,479×Mn>−9,860  <2> 811×C+135×Mn+602×Ti+794×Nb>465  <3>, and having strength of at least 980 N/mm². (2) A high-strength hot-rolled steel sheet excellent in hole expandability and ductility, containing in terms of a mass %:

C: 0.01 to 0.09%,

Si: 0.05 to 1.5%,

Mn: 0.5 to 3.2%,

Al: 0.003 to 1.5%,

P: 0.03% or below,

S: 0.005% or below,

Ti: 0.10 to 0.25%,

Nb: 0.01 to 0.05%,

at least one of

Mo: 0.05 to 0.40% and V: 0.001 to 0.10%, and

the balance consisting of iron and unavoidable impurities;

satisfying all of the following formulas <1>′ to <3>′: 0.9≦48/12×C/Ti<1.7  <1>′ 50,227×C−4,479×(Mn+0.57×Mo+1.08×V)>−9,860  <2>′ 811×C+135×(Mn+0.57×Mo+1.08×V)+602×Ti+794×Nb>465  <3>′, and having strength of at least 980 N/mm². (3) A high-strength hot-rolled steel sheet excellent in hole expandability and ductility according to (1) or (2), which further contains, in terms of mass %, 0.0005 to 0.01% of at least one of Ca, Zr and REM. (4) A high-strength hot-rolled steel sheet excellent in hole expandability and ductility according to any of (1) through (3), which further contains, in terms of mass %, 0.0005 to 0.01% of Mg. (5) A high-strength hot-rolled steel sheet excellent in hole expandability and ductility according to any of (1) through (4), which further contains, in terms of mass %, at least one of:

Cu: 0.1 to 1.5% and

Ni: 0.1 to 1.0%.

(6) A production method of a high-strength hot-rolled steel sheet excellent in hole expandability and ductility according to any of (1) through (5), comprising the steps of:

finishing hot rolling by setting a rolling finish temperature to from an Ar₃ transformation point to 950° C.;

cooling the hot-rolled steel sheet to 650 to 800° C. at a cooling rate of at least 20° C./sec;

cooling then the steel sheet for 0.5 to 15 seconds;

further cooling the steel sheet to 300 to 600° C. at a cooling rate of at least 20° C./sec; and

coiling the steel sheet.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a graph showing the effects, in a steel of the invention, on elongation with respect to tensile strength; and

FIG. 2 is a graph showing the effects, in the steel of the invention, on an hole expansion ratio with respect to tensile strength.

BEST MODE FOR CARRYING OUT THE INVENTION

It is known, in high-strength steel sheets, that elongation and hole expandability are deteriorated with an increase in strength and the hole expandability and ductility are contradictory. To solve the problem, the inventors of the invention have conducted intensive studies and have found that elongation and hole expandability can be improved with high strength by stipulating the ranges of C, Mn and Ti components. The invention has thus been completed. In other words, the inventors have derived relational formulas by clarifying the influences of maximum utilization of precipitation hardening of TiC and structure strengthening by Mn and C on materials and have solved the problems described above.

The reason for stipulation of each element of the steel composition will be hereinafter explained.

C is limited to 0.01 to 0.09%. C is an element necessary for precipitating carbides and securing the strength. When the C content is less than 0.01%, a desired strength cannot be secured easily. When the C content exceeds 0.09%, the effect of increasing the strength disappears and, moreover, ductility is deteriorated. Therefore, the upper limit is set to 0.09%. Preferably, C is 0.07% or smaller because it is the element that invites deterioration of hole expandability.

Si is an element that improves strength by solid solution hardening, promotes ferrite formation by suppressing the formation of detrimental carbides, is important for improving elongation and can satisfy both strength and ductility. To acquire such effects, at least 0.05% of Si must be added. When the addition amount increases, however, a de-scaling property resulting from Si scales and the ability of phosphate coating drop. Therefore, the upper limit is set to 1.5%. Incidentally, the range of Si is preferably from 0.9 to 1.3% to simultaneously satisfy the hole expandability and ductility.

Mn is one of the important elements in the invention. Though Mn is necessary for securing strength, it deteriorates elongation. Therefore, the Mn content is as small as possible as long as the strength can be secured. Particularly when a large amount of Mn beyond 3.2% is added, micro segregation and macro segregation are more likely to occur and the hole expandability is remarkably deteriorated. Therefore, the upper limit is set to 3.2%. Particularly when elongation is of importance, the Mn content is preferably 3.0% or below. On the other hand, Mn has a function of making S that is detrimental for the hole expandability harmless as Mn. To obtain such an effect, at least 0.5% of Mn must be added.

Al is effective as a deoxidizer, suppresses the formation of detrimental carbides and promotes the ferrite formation in the same way as Si and improves elongation, so that both strength and ductility can be satisfied. When used as the deoxidizer, at least 0.003% of Al must be added. When the Al content exceeds 1.5%, on the other hand, the ductility improvement effect is saturated. Therefore, the upper limit is set to 1.5%. Because the addition of a large amount of Al lowers cleanness of the steel, the Al content is preferably 0.5% or below.

P undergoes solid solution in a ferrite and lowers ductility. Therefore, its content is limited to 0.03% or below.

S forms MnS, operates as the starting point of destruction and remarkably lowers hole expandability as well as ductility. Therefore, its content is limited to 0.005% or below.

Ti is one of the most important elements in the invention and is effective for securing strength through precipitation of TiC. Degradation of elongation by Ti is smaller than Mn and, Ti is used effectively. To obtain this effect, at least 0.10% of Ti must be added. When a large amount of Ti is added, on the other hand, precipitation of TiC proceeds during heating for hot rolling and Ti does not contribute any longer to the strength. Therefore, the upper limit is set to 0.25% at the upper limit of the existing heating temperature.

Nb is an element effective for securing the strength through NbC precipitation in the same way as the addition of Ti. Because degradation of elongation is less in comparison with Mn, Nb is used effectively. To obtain this effect, at least 0.01% of Nb must be added. However, because the addition effect is saturated even when 0.05% or more of Nb is added, the upper limit is set to 0.05%.

Mo is an element that contributes to the improvement of strength in the same way as Mn but lowers elongation. Therefore, its addition amount is preferably small as long as the strength can be secured. Particularly, when the Mo content exceeds 0.40%, the drop of ductility becomes great and the upper limit is therefore set to 0.40%. When Mo is added as a partial substitute for Mn, it can mitigate Mn segregation. To obtain this effect, at least 0.05% of Mo must be added.

V is an element that contributes to the improvement of strength in the same way as Mo and Mn but deteriorates elongation. Therefore, the addition amount of V is preferably small as long as the strength can be secured. Further, when the V content exceeds 0.10%, cracking is likely to occur during casting. Therefore, the upper limit is set to 0.10%. V can mitigate Mn segregation when added as a partial substitute for Mn. To obtain this effect, at least 0.001% of B must be added.

Ca, Zr and REM are effective elements for controlling the form of sulfide type inclusions and improving the hole expandability. To render this controlling effect useful, at least 0.0005% of at least one kind of Ca, Zr and REM is preferably added. On the other hand, the addition of a greater amount invites coarsening of the sulfide type inclusions, deteriorates cleanness, lowers ductility and invites the cost of production. Therefore, the upper limit is set to 0.01%.

When added, Mg combines with oxygen and forms oxides. The inventors of this invention have found that refinement of MgO or composite oxides of Al₂O₃, SiO₂, MnO and Ti₂O₃ containing MgO formed at this time lets them have smaller sizes as individual oxides and have a uniform dispersion state. Though not yet clarified, these oxides finely dispersed in the steel form fine voids at the time of punching, contribute to the dispersion of the stress and suppress the stress concentration to thereby suppress the occurrence of coarse cracks and to improve the hole expandability. However, the effect of Mg is not sufficient when its content is less than 0.0005%. When the content exceeds 0.01%, the improvement effect is saturated and the production cost increases. Therefore, the upper limit is set to 0.01%.

Cu and Ni are the elements that improve hardenability. These elements are effective for securing the second phase percentage and the strength when added particularly at the point at which a cooling rate is low so as to control the texture. To make this effect useful, at least 0.1% of Cu or at least 0.1% of Ni is preferably added. However, the addition of these elements in greater amounts promotes degradation of ductility. Therefore, the upper limit of Cu is 1.5% and 1.0% for Ni.

The steel does not come off from the range of the invention even when it contains, as unavoidable impurity elements, not greater than 0.01% of N, less than 0.1% of Cu, less than 0.1% of Ni, not greater than 0.3% of Cr, less than 0.05% of Mo, not greater than 0.05% of Co, not greater than 0.05% of Zn, not greater than 0.05% of Sn, not greater than 0.02% of Na and not greater than 0.0005% of B, for example.

As a result of intensive studies for solving the problems described above, the inventors of this invention have found that elongation and the hole expandability can be improved, with high strength, by stipulating the ranges of C, Mn and Ti components. In other words, the present inventors have derived the following three relational formulas by clarifying the influences of maximum utilization of TiC precipitation hardening and texture strengthening by Mn and C on the materials. The relational formulas will be hereinafter explained.

When the addition amount of C is smaller than that of Ti, solid solution Ti increases and deteriorates elongation. Therefore, the relation 0.9≦48/12×C/Ti is stipulated. On the other hand, when the C content is excessively greater than the Ti content, TiC precipitates during heating for hot rolling and the increase of the strength cannot be obtained. In addition, the hole expandability is deteriorated due to the increase of the C content in the second phase. Therefore, the relation 48/12×C/Ti <1.7 is set. In other words, the following formula <1>must be satisfied. Particularly when the hole expandability is important, the relation 1.0<48/12×C/Ti <1.3 is preferably satisfied. 0.9≦48/12×C/Ti<1.7  <1>

The formation of ferrite is suppressed with the increase of the addition amount of Mn. Consequently, the second phase percentage increases and the strength can be secured more easily but the drop of elongation occurs. Elongation can be improved, though the hole expandability drops, by hardening the second phase. Therefore, to secure elongation of at least 980 N/mm², the following formula <2>must be satisfied: 50,227×C−4,479×Mn>−9,860  <2>

Since the effect of each of Mo and V is determined by its atomic equivalent at this time, the formula <2>changes to <2>′ under the condition in which Mo or V is added: 50,227×C−4,479×(Mn+0.57×Mo+1.08×V)  <2>′

To secure workability, the two formulas described above must be satisfied. It is relatively easy in the steel sheets of a 780 N/mm² level to satisfy these two formulas while securing the strength. To secure the strength exceeding 980 N/mm², however, it is unavoidable to add C that deteriorates the hole expandability and Mn that deteriorates elongation. Therefore, to secure the strength exceeding 980 N/mm², it is necessary to adjust the components so as to satisfy the range of the following formula <3>while satisfying the two formulas described above: 811×C+135×Mn+602×Ti+794×Nb >465  <3>

As the effect of each of Mo and V is determined by its atomic equivalent at this time, the formula <3>changes to <3>′ under the condition in which Mo or V is added: 811×C+135×(Mn+0.57×Mo+1.08×V)+602×Ti+794×Nb >465  <3>′

When a high-strength hot-rolled steel sheet is produced by hot rolling, the finish rolling end temperature must be higher than the Ar₃ transformation point to suppress the formation of ferrite and to improve the hole expandability. When the temperature is raised excessively, however, the drop of the strength and ductility occurs owing to coarsening of the texture. Therefore, the finish rolling end temperature must be not higher than 950° C.

To acquire the high hole expandability, it is important to rapidly cool the steel sheet immediately after the end of the rolling and the cooling rate must be at least 20° C./sec. When the cooling rate is less than 20° C./sec, it becomes difficult to suppress the formation of carbides that are detrimental to the hole expandability.

Rapid cooling of the steel sheet is thereafter stopped once and air cooling is applied in the invention. This is important to increase the occupying ratio of ferrite by precipitating it and to improve ductility. However, pearlite, that is detrimental to the hole expandability, occurs from an early stage when the air cooling start temperature is less than 650° C. When the air cooling start temperature exceeds 800° C., on the other hand, the formation of ferrite is slow. Therefore, not only the air cooling effect cannot be obtained easily but the formation of pearlite is likely to occur during subsequent cooling. For this reason, the air cooling start temperature is from 650 to 800° C. The increase of ferrite is saturated even when the air cooling time is longer than 15 seconds and loads are applied to subsequent cooling rate and control of a coiling temperature. Therefore, the air cooling time is not longer than 15 seconds. When the cooling time is less than 0.5 seconds, the formation of ferrite is not sufficient and the effect of improvement of elongation cannot be obtained. The steel sheet is again cooled rapidly after air cooling and the cooling rate must be at least 20° C./sec, too. This is because, detrimental pearlite is likely to be formed when the cooling rate is less than 20° C./sec.

The stop temperature of this rapid cooling, that is, the coiling temperature, is set to 300 to 600° C. This is because, martensite, that is detrimental to the hole expandability, occurs when the coiling temperature is less than 300° C. When the coiling temperature exceeds 600° C., on the other hand, pearlite and cementite that are detrimental to the hole expandability, are more easily formed.

A high-strength hot-rolled steel sheet excellent in workability and having a strength of higher than 980 N/mm² can be produced by combining the components and the rolling condition described above. When surface treatment (for example, zinc coating) is applied to the surface of the steel sheet according to the invention, such a steel sheet has the effects of the invention and does not leave the scope of the invention.

EXAMPLES

Next, the invention will be explained with reference to examples thereof.

Steels having components tabulated in Table 1 and Table 2 (continuing Table 1) are molten and continuously cast into slabs in a customary manner. Symbols A to Z represent the steels having the components of the invention. Steel having a symbol a has a Mn addition amount outside the range of the invention. Similarly, steel b and steel d have a Ti addition amount and a C addition amount outside the ranges of the invention, respectively. Further, steel having a symbol C has values of formulas <1>and <3>outside the range of the invention. These steels are heated at a temperature higher than 1,250° C. in a heating furnace and are hot rolled into hot-rolled steel sheets having a sheet thickness of 2.6 to 3.2 mm. The hot rolling condition is tabulated in Table 3 and Table 4 (continuing Table 3).

In Table 3 and Table 4 (continuing Table 3), C3 has a coiling temperature outside the range of the invention. Similarly, J2 has an air cooling start temperature outside the range of the invention, P3 has a finish temperature outside the range of the invention and S3 has a coiling temperature outside the range of the invention.

Each of the resulting hot-rolled steel sheets is subjected to a tensile test by using a JIS No. 5 test piece and a hole expansion test. As for the hole expandability, a hole expansion ratio λ=(d−d_(o))/d×100 is evaluated.

The ratio is obtained from a hole diameter (d) formed when a crack perforates through the sheet thickness while expanding a punched hole having a diameter of 10 mm using a 60 conical punch and an initial hole diameter (d_(o): 10 mm).

Table 3 and Table 4 (continuing Table 3) tabulate the tensile strength TS, elongation E1 and the hole expansion ratio λ of each test piece. FIG. 1 shows the relation between the strength and elongation and FIG. 2 shows the relation between the strength and the hole expansion ratio. It can be understood that the steels of the invention have a higher elongation or a better hole expansion ratio than Comparative Steels. It can thus be understood that the steel sheets according to the invention have both an excellent hole expansion ratio and good ductility. TABLE 1 C Si Mn P S N Al Nb Ti Mo V Mg other steel wt % A 0.06 1.3 2.5 0.007 0.002 0.003 0.04 0.035 0.17 — — — Ca: 0.003 B 0.05 1.0 2.2 0.006 0.001 0.004 0.03 0.035 0.17 — — — Ca: 0.003 C 0.06 1.4 2.8 0.006 0.001 0.002 0.03 0.012 0.14 — — — Ca: 0.003 D 0.03 1.3 2.5 0.006 0.001 0.003 0.03 0.040 0.12 — — — — E 0.05 0.4 2.1 0.006 0.001 0.002 0.44 0.048 0.18 — — — — G 0.10 1.5 1.6 0.007 0.001 0.003 0.04 0.048 0.25 — — — Zr: 0.002 H 0.05 1.3 2.3 0.025 0.001 0.003 0.04 0.038 0.16 — — — — I 0.05 1.0 2.5 0.006 0.004 0.003 0.04 0.035 0.15 — — — Ca: 0.003 J 0.04 1.3 2.3 0.005 0.001 0.003 0.04 0.040 0.16 — — — — K 0.07 1.0 2.8 0.005 0.001 0.003 0.04 0.040 0.19 — — — — L 0.07 1.0 2.4 0.005 0.001 0.003 0.04 0.035 0.19 — — — — M 0.06 1.0 2.3 0.005 0.001 0.003 0.04 0.040 0.19 — — — — N 0.08 1.2 1.9 0.007 0.001 0.004 0.04 0.040 0.21 — — — — O 0.08 1.2 2.2 0.007 0.001 0.004 0.04 0.040 0.22 — — — Cu: 0.4, Ni: 0.2 P 0.05 1.3 2.4 0.007 0.003 0.004 0.04 0.040 0.15 — — — REM: 0.003 Q 0.05 1.3 2.4 0.007 0.002 0.004 0.04 0.040 0.15 — 0.05 — — R 0.05 1.3 2.4 0.007 0.002 0.004 0.04 0.040 0.15 0.17 — — Ca: 0.003 S 0.05 1.3 2.4 0.007 0.003 0.004 0.04 0.040 0.15 0.32 — — — T 0.06 1.3 2.4 0.007 0.002 0.003 0.04 0.035 0.17 — — 0.004 — U 0.05 1.0 2.2 0.006 0.001 0.004 0.03 0.035 0.17 — — 0.002 — V 0.03 1.3 2.5 0.006 0.001 0.003 0.03 0.040 0.12 — — 0.002 — W 0.07 1.3 1.8 0.007 0.001 0.003 0.04 0.048 0.22 — — 0.008 Ca: 0.003 X 0.08 1.2 1.9 0.007 0.001 0.004 0.04 0.040 0.21 — — 0.004 — Y 0.08 1.2 2.2 0.007 0.001 0.004 0.04 0.040 0.22 — — 0.004 0 Z 0.05 1.2 2.3 0.007 0.002 0.004 0.04 0.040 0.15 0.17 — 0.005 Ca: 0.003 a 0.05 1.2 3.5 0.007 0.002 0.004 0.04 0.040 0.15 — — — — b 0.08 1.2 2.0 0.007 0.002 0.004 0.04 0.040 0.30 — — — — c 0.08 1.2 1.5 0.007 0.002 0.004 0.04 0.040 0.15 — — — — d 0.20 1.2 1.6 0.007 0.002 0.004 0.04 0.040 0.15 — — — — *Ar₃ = 900 − 510C + 28Si − 50Mn + 229Ti An underline indicates that the steel is outside the range of the invention.

TABLE 2 (continuing Table 1) formula <1> formula intermediate <2> formula <3> Ar₃ steel term left term left term ° C. remarks A 1.3 −8435 512 823 inventive steel B 1.2 −7342 468 831 inventive steel C 1.6 −9779 513 803 inventive steel D 1.0 −9780 466 822 inventive steel E 1.0 −7095 467 824 inventive steel G 1.6 −2144 485 867 inventive steel H 1.3 −7790 478 833 inventive steel I 1.3 −8686 496 812 inventive steel J 1.0 −8293 468 837 inventive steel K 1.5 −9025 581 797 inventive steel L 1.5 −7234 523 817 inventive steel M 1.3 −7288 505 827 inventive steel N 1.5 −4542 479 847 inventive steel O 1.4 −5936 524 835 inventive steel P 1.3 −8238 487 826 inventive steel Q 1.3 −8480 494 826 inventive steel R 1.3 −8667 500 826 inventive steel S 1.3 −9055 511 826 inventive steel T 1.3 −7987 499 828 inventive steel U 1.2 −7342 468 832 inventive steel V 1.0 −9780 466 822 inventive steel W 1.3 −4546 470 862 inventive steel X 1.5 −4542 479 847 inventive steel Y 1.4 −5936 524 835 inventive steel Z 1.3 −8219 486 828 inventive steel a 1.3 −13165  635 768 comparative steel b 1.1 −4940 547 862 comparative steel c 2.1 −2700 389 853 comparative steel d 5.3   2879 500 788 comparative steel *Ar₃ = 900 − 510C + 28Si − 50Mn + 229Ti An underline indicates that the steel is outside the range of the invention.

TABLE 3 air finish cooling air cooling cooling coiling tensile temperature rate start time temperature strength hole steel ° C. ° C./s temperatures ° C. ° C. N/mm² elongation % expansion % remarks A1 853 50 700 3 500 1040 13.9 57 inventive steel A2 880 33 740 0.8 550 1050 13.7 62 inventive steel A3 830 42 780 14 580 995 14.5 50 inventive steel B1 861 44 700 3 550 992 15.6 64 inventive steel B2 930 61 650 3 500 1002 14.5 64 inventive steel B3 880 33 760 0.7 550 987 15.2 70 inventive steel C1 833 59 670 4 480 1042 12.5 48 inventive steel C2 850 44 670 2 500 1052 12.4 48 inventive steel C3 860 83 700 1.5  30 1037 12.1 30 comparative steel D1 852 57 680 3 450 994 13.2 71 inventive steel E1 854 38 700 2 550 986 16.0 73 inventive steel F1 897 55 680 3 510 1014 20.4 50 inventive steel G1 863 86 680 4 350 1006 15.0 55 inventive steel H1 842 50 670 3 490 1021 13.9 57 inventive steel I1 867 40 680 2 550 996 14.6 71 inventive steel J1 827 47 680 3 500 1106 12.5 50 inventive steel J2 880 80 820 5 480 1096  7.0 50 comparative steel L1 847 59 680 5 550 1048 14.9 52 inventive steel M1 857 51 660 3 500 1030 15.1 59 inventive steel N1 877 97 630 6 490 1006 18.2 53 inventive steel An underline indicates that the steel is outside the range of the invention.

TABLE 4 (continuing Table 3) air finish cooling air cooling cooling coiling tensile temperature rate start time temperature strength hole steel ° C. ° C./s temperatures ° C. ° C. N/mm² elongation % expansion % remarks O1 865 30 720 0.6 580 1051 16.1 53 inventive steel P1 856 51 680 3 500 1015 14.4 57 inventive steel P2 900 70 700 5 550 1025 14.3 57 inventive steel P3 780 30 680 0.6 480  900 14.0 68 comparative steel Q1 856 51 670 4 550 1022 14.1 57 inventive steel R1 856 34 700 2 580 1028 13.8 57 inventive steel S1 856 51 670 4 550 1039 13.3 56 inventive steel S2 840 25 680 0.6 590 1049 12.7 50 inventive steel S3 900 36 670 3 650 1079 13.3 25 comparative steel T1 858 112 680 5 300 1027 14.5 78 inventive steel T2 900 88 720 6 550 1037 14.3 78 inventive steel T3 880 33 700 0.6 550 1022 14.1 83 inventive steel U1 862 76 700 5 480  993 15.6 84 inventive steel V1 852 50 670 3 500  994 13.2 91 inventive steel V2 880 47 700 3 550 1004 13.0 90 inventive steel V3 840 47 680 3 510  989 13.2 91 inventive steel W1 892 49 700 3 550  998 18.3 80 inventive steel X1 877 55 670 3 490 1006 18.2 73 inventive steel Y1 865 45 700 3 550 1051 16.1 73 inventive steel Z1 858 51 680 3 500 1013 14.5 77 inventive steel a1 798 31 700 2 550 1162  5.3 51 comparative steel b1 892 57 720 4 550  912 12.0 75 comparative steel c1 883 62 670 4 510  916 22.0 44 comparative steel d1 818 33 740 2 550  900 28.6 26 comparative steel An underline indicates that the steel is outside the range of the invention.

INDUSTRIAL APPLICABILITY

As described above in detail, the invention can economically provide a high-strength hot-rolled steel sheet having a tensile strength of at least 980 N/mm² and satisfying both an hole expandability and ductility. Therefore, the invention is suitable as a high-strength hot-rolled steel sheet having high workability. The high-strength hot-rolled steel sheet according to the invention can reduce the weight of a car body, can achieve integral molding of components and rationalization of a production process, can improve a fuel efficiency and can reduce the production cost. Therefore, the invention has large industrial value. 

1. A high-strength hot-rolled steel sheet excellent in hole expandability, and ductility, containing in terms of a mass %: C, 0.01 to 0.09%, Si: 0.05 to 1.5%, Mn: 0.5 to 3.2%, Al: 0.003 to 1.5%, P: 0.03% or below, S: 0.005% or below, Ti: 0.10 to 0.25%, Nb: 0.01 to 0.05%, and the balance consisting of iron and unavoidable impurities; satisfying all of the following formulas <1>to <3>: 0.9<48/12×C/Ti<1.7  <1> 50,227×C−4,479×Mn>−9,860  <2> 811×C+135×Mn+602×Ti+794×Nb>465  <3>, and having strength of at least 980 N/mm².
 2. A high-strength hot-rolled steel sheet excellent in hole expandability and ductility, containing in terms of a mass %: C, 0.01 to 0.09%, Si: 0.05 to 1.5%, Mn: 0.5 to 3.2%, Al: 0.003 to 1.5%, P: 0.03% or below, S: 0.005% or below, Ti: 0.10 to 0.25%, Nb: 0.01 to 0.05%, at least one of Mo: 0.05 to 0.40% and V:0.001 to 0.10%, and the balance consisting of iron and unavoidable impurities; satisfying all of the following formulas <1>′ to <3>′: 0.9≦48/12×C/Ti<1.7  <1>′ 50,227×C−4,479×(Mn+0.57×Mo+1.08×V)>−9,860  <2>′ 811×C+135×(Mn+0.57×Mo+1.08×V)+602×Ti+794×Nb>465  <3>, and having strength of at least 980 N/mm².
 3. A high-strength hot-rolled steel sheet excellent in hole expandability and ductility according to claim 1, which further contains, in terms of mass %, 0.0005 to 0.01% of at least one of Ca, Zr and REM.
 4. A high-strength hot-rolled steel sheet excellent in hole expandability and ductility according to claim 1, which further contains, in terms of mass %, 0.0005 to 0.01% of Mg.
 5. A high-strength hot-rolled steel sheet excellent in hole expandability and ductility according to claim 1, which further contains, in terms of mass %, at least one of: Cu: 0.1 to 1.5% and Ni: 0.1 to 1.0%.
 6. A production method of a high strength hot rolled steel sheet excellent in hole expandability and ductility according to claim 1, comprising the steps of: finishing hot rolling by setting a rolling end temperature to from an Ar₃ transformation point to 950° C.; cooling a hot rolled steel sheet to 650 to 800° C. at a cooling rate of at least 20° C./sec; air cooling then the steel sheet for 0.5 to 15 seconds; further cooling the steel sheet to 300 to 600° C. at a cooling rate of at least 20° C./sec; and coiling the steel sheet. 